ADG-210 is an attitude determination system for various platforms. ADG-210 provides attitude, angular velocity and linear acceleration to the host vehicle systems continuously.
ADG-210 consists of strap down inertial measurement unit, system processor unit, power supply unit and chassis.
ADG-210 is a cost effective solution for all types of platforms requiring attitude during their mission.
ADG-210 is an open architecture and hardware/ software flexible unit which can be adapted to various platforms.
Long mean time between failure (MTBF) and internal built in test capability reduces the logistics requirement to a minimum. ADG-210 does not require periodic maintenance.
Roll, Pitch And Yaw Angle Outputs
Angular Rate Output
Linear Acceleration Output
Low Power Dissipation (12 W, 28 VDC)
Built-In Test Capability
Field Programmable Software
No Periodic Maintenance
System Operational Modes
Continuous Output Mode
Polled Output Mode
MIL-STD-704F Electrical Power Interface
RS422 Serial User Interface
High Speed RS422 Asynchronous Serial Test Interface
Parameter Performance Specifications
Yaw Angle (long term period) 20 deg / hour
Yaw Angle (short term period) 0.5 deg
Roll and Pitch Angle (long term period) 1 deg
Roll and Pitch Angle (short term period) 0.5 deg
Angular Rate (x, y, z) 0.25 deg / sec
Accelerometer Bias (x, y, z) 24 mg
Electromagnetic Environmental Effects
Dimensions: 152 mm (H) x 127 (D) x 109 mm (W) (without connector)
Weight: <2 kg